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Weak form quadrature element analysis on nonlinear bifurcation and post- buckling of cylindrical composite laminates

机译:圆柱复合材料层合板非线性分叉和后屈曲的弱形式正交元分析

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This paper presents a weak form quadrature element formulation in the analysis of nonlinear bifurcation and post-buckling of cylindrical composite laminates subjected to transverse loads. A total Lagrangian updating scheme is used in combination with arc-length method and the branch switching method is adopted to identify the whole post-buckling procedure of the laminates. The formulation of the shell model is based on the basic concept of Ahmad. The coincidence of discrete nodes and integration points in quadrature element endows it with compactness and conciseness in the nonlinear buckling analysis of cylindrical laminates. Shear and membrane locking problems are avoided in the quadrature element formulation for its high-order approximation property. Several numerical examples are firstly presented to verify the effectiveness and accuracy of the present formulation. Parametric studies of the effects including rise, thickness, boundary conditions and lamination scheme of the cylindrical composite laminates on the bifurcation and post-buckling behaviors are performed.
机译:本文在分析承受横向载荷的圆柱形复合材料层合板的非线性分叉和后屈曲时,提出了一种弱形式的正交单元公式。采用总的拉格朗日更新方案与弧长法相结合,并采用分支切换法来识别层压板的整体后屈曲过程。壳模型的建立基于Ahmad的基本概念。正交单元中离散节点和积分点的重合使圆柱层压板的非线性屈曲分析具有紧凑性和简洁性。由于正交近似的高阶近似特性,避免了剪切和膜锁定问题。首先给出几个数值例子,以验证本发明配方的有效性和准确性。对包括圆柱形复合材料层压板的上升,厚度,边界条件和层压方案对分叉和后屈曲行为的影响进行了参数研究。

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